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0 Hz 3 Combustor inlet 1 Throat Nozzle Exit Oxygen (gas) and hydrogen (gas) inlet temperatures are equal to 25 C Combustor pressure (same

- Oxygen (gas) and hydrogen (gas) inlet temperatures are equal to ( 25 mathrm{C} ) - Combustor pressure (same as inlet (

Determine - The balanced chemical reactions for equivalence ratio ( (mathrm{phi}=0.2,1.0 ) and ( 2.0) )  
 

0 Hz 3 Combustor inlet 1 Throat Nozzle Exit Oxygen (gas) and hydrogen (gas) inlet temperatures are equal to 25 C Combustor pressure (same as inlet H2 and 02 pressure, and nozzle inlet pressure) = 20MPa The nozzle exhausts in an atmosphere whose pressure is 100 kPa Determine The balanced chemical reactions for equivalence ratio (phi= 0.2, 1.0 and 2.0)

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